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2015 NATOPS Manual Change Summary 2015 NATOPS Manual Change Summary

2015 NATOPS Manual Change Summary - PowerPoint Presentation

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2015 NATOPS Manual Change Summary - PPT Presentation

Purpose To provide changes on major changes to the TH57BC NATOPS Manual This training is not all inclusive and only consists of the major changes Revision should be read cover to cover Terminology and Layout ID: 727725

major chapter added check chapter major check added oil natops engine required failure considered procedure criteria cover read manual

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Slide1

2015 NATOPS Manual Change SummarySlide2

Purpose

To provide changes on major changes to the TH-57B/C NATOPS Manual.

This training is not all inclusive and only consists of the major changes.

Revision should be read cover to cover.Slide3

Terminology and Layout

Terminology

FCS

SMA

SEBD

Multiple changes to grammar and wording

Stylistic changes to multiple Notes, Warnings and Cautions

Layout

Preface and Chapter One have been standardized by NAVAIR

Changes to Preface will not be entertainedSlide4

Chapter Two

Major overhaul of MINISTAB system description

Associated new MINSTAB terminology

RADALT referred to as the KRA-405(series)

Old reference to seats with “adjustable lumbar” removedSlide5

Chapter Three

New primary/alternate fluids for Hydraulic System, Rotor Brake and Main Rotor Hub Grips

New protocol for servicing Engine Oil

Requirement to dry motor for 30 seconds before checking oil level to service

Reference to the “inside edge of the cap adapter” aka Weld Line for servicing only.

Do use the dipstick to check the fluid level.Slide6

Chapter Four

Intentional operation in the transient range of any limit is prohibited.

Minimum fuel reserve requirement is 10 gallons

Steady State

Nf

defined

Ng at idle now 63+/- 1%

Gauge images now only contain the gauge markings (no limits)

Power off Nr transient range eliminated

Crew requirement added for CAL/Externals

Prohibited Maneuvers changed:

“Intentional entry into Vortex Ring State” changed to “Fully developed Vortex Ring State”

60 degrees angle of bank removed

Aerobatic maneuvers still prohibited. AOB greater than 60 are considered aerobaticSlide7

Chapter Six

All NATOPS brief items consolidated into Chapter Six

Dynamic Rollover added as a NATOPS brief item

Special Instructions for Shipboard Ops and NVDs are spelled out in the NATOPS manual, but are only a bullet in the PCL.Slide8

Chapter Seven

Tail Rotor Oil-Check for visible oil level vice 1/8” above line.

Major change to start sequence

Deceleration and Flight Idle check required for both twist grips

Hydraulics check no longer its own check, now at the end of the

Pretakeoff

checks as a daggered item.Slide9

Chapter Nine

Major revisions to practice autorotation maneuver descriptions

“Slow to Spool” alluded to

15 second wait following power off maneuvers no longer required

Stability language still exists (

Nf

/Nr 60-65, Ng stabilized in idle range)

Neutralizing pedals still required

Still not allowed to exceed 40% torque on the run-up

Voice procedures for tactics addedSlide10

Chapter Ten

Come find me if you’re interested.Slide11

Chapter Eleven

Large discussion of

autorotative

aerodynamics added.

Written by HITU IPs, meant to be readable and accessible for students

Please read it and have your students read it as well

Minor changes to dynamic rollover section

Discussion of LTE modified slightlySlide12

Chapter Twelve

Failures may not be accompanied by every indication

FUEL LOW/FUEL PRESS

ENG OUT light identified as engine or

tach

-gen failure

ENG CHIP delineated as “third or fourth” vice “any subsequent” chip

TRANS CHIP maintenance criteria elaborated uponSlide13

Chapter Thirteen

Abort Start criteria elaborated

Battery voltage stabilized below 17 volts

Engine Oil pressure remains at 0

Rotors not turning by 25% Ng

Transmission Oil Pressure not indicated by 30% Nr

All old criteria remainSlide14

Chapter Fourteen

Restart-as required added to Engine Failure in Flight

Collective-Lower standardized

Compressor Stall procedure modified

Engine Restart procedure modified

Tail Rotor AUTHORITY may be lost if

Nf

is allowed to go below 80%.

Shoulder Harness standardized

Main Generator Failure and

Loadmeter

/Voltmeter malfunction consolidated into one procedure

Landing criteria eliminated from Smoke/Fume Elimination

Directional Gyro Failure guidance providedSlide15

Chapters Fifteen and Sixteen

Major overhaul to autorotation/egress EPs

BAD NEWS

No longer the fleet underwater egress procedure

GOOD NEWS!

Much shorter and user friendlySlide16

Miscellaneous

Chapter Seventeen

SWEEP check added and defined

Chapter Twenty-One: NATOPS Evaluations

Preflight no longer considered critical

Power Recovery Autorotation is considered critical

All items considered critical SHALL be

performed

PCL

Changes to names of tabs

Wind envelopes removedSlide17

What’s coming next?

Read the manual cover to cover

If you have discrepancies, changes to recommend, DO IT NOW.

Email me and I will submit it for you to Wing.

Expanded checklist and briefing guide to be a signed instruction.

RWOP revisionSlide18

QUESTIONS??